# N282SK: 2001 Embraer EMB-145LR, registration cancelled 2019-10-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 9, 2019
- Exported to: Bahamas
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212)
- Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145409
- Year built: 2001
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 3, 2001
- Last registry action: October 9, 2019
- Mode S code: A2D703
- Owner when cancelled: [Enterprise Lease Finance LLC](https://openairdocs.org/faa-owner/ENTERPRISE%20LEASE%20FINANCE%20LLC)
- Location: [Saint Louis, MO](https://openairdocs.org/faa-place/MO/Saint%20Louis)
- Owner type: LLC
- Owner's area on the map: 38.6443° N, 90.3281° W: Placed by OpenAirDocs at the center of ZIP code 63105, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N282SK
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=282SK
- Page: https://openairdocs.org/deregistered/N282SK-2019-10-09

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer EMB-145LR: https://openairdocs.org/model/embraer-emb-145lr.md

## Service difficulty reports (45)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR UHLA201606010290](https://openairdocs.org/sdr/UHLA201606010290), Jun 1, 2016: GATE. OUT OF ADJUST. MAIN CABIN DOOR HAS LARGE GAP AT TOP SEAL. RED ALIGN MARKS SLIGHTLY OFF. ADJUSTED MAIN CABIN DOOR FOLDING FLAP IAW AMM 52-10-01.
- [SDR UHLA201605170245](https://openairdocs.org/sdr/UHLA201605170245), May 17, 2016: SPRING. BROKEN. NR 3 AIRSTAIR STEP SPRING BROKE. R & R SPRING IAW AMM 52-10-07.
- [SDR UHLA201605160248](https://openairdocs.org/sdr/UHLA201605160248), May 16, 2016: WIRE. DAMAGED. GALLEY SERVICE DOOR INDICATES OPEN WHEN SECURED CLOSED AND VERIFIED CLOSED. REPAIRED WIRE ON DOOR HARNESS IAW SRPM.
- [SDR CHQA20140424123](https://openairdocs.org/sdr/CHQA20140424123), Apr 24, 2014: PROXIMITY SWITCH. FAULTY. CREW REPORTED THAT THEY RECEIVED A LG AIR & GND FAIL MSG IN FLIGHT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. FOUND THE NLG WEIGHT ON WHEELS SWITCH 
- [SDR CHQA20140418111](https://openairdocs.org/sdr/CHQA20140418111), Apr 18, 2014: STRUT. UNDERSERVICED. CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LG AIR & GND FAIL MSG. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT. THE ACFT WAS FOUND SAFE FOR FERRY 
- [SDR CHQA20140407109](https://openairdocs.org/sdr/CHQA20140407109), Apr 7, 2014: WIRE HARNESS. FAULTY. CREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED A LG AIR & GND FAIL MSG & THAT THE LG DID NOT RETRACT. THE CREW ELECTED TO RETURN TO FIELD & LANDED WITHOUT INCI
- [SDR CHQA20140331099](https://openairdocs.org/sdr/CHQA20140331099), Mar 31, 2014: ELECTRONIC UNIT. FAULTY. CREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED A LG AIR & GND FAIL MSG & THAT THE LG DID NOT RETRACT. THE CREW ELECTED TO RETURN TO FIELD & LANDED WITHOUT INCI
- [SDR CHQA20140324092](https://openairdocs.org/sdr/CHQA20140324092), Mar 24, 2014: PROXIMITY SWITCH. FAULTY. CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LG AIR & GND FAIL MESSAGE & THAT THE LG WOULD NOT RETRACT. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT
- [SDR CHQA20131212445](https://openairdocs.org/sdr/CHQA20131212445), Dec 12, 2013: WINDSHIELD. CRACKED. CREW REPORTED THAT DURING CLIMB, THE CAPTAIN`S WINDSHIELD CRACKED. THE CREW DECLARED AN EMERGENCY & RETURNED TO FIELD. MX REPLACED THE LT WINDSHIELD. OPERATIONA
- [SDR CHQA20130904337](https://openairdocs.org/sdr/CHQA20130904337), Sep 4, 2013: WIRE. INOPERATIVE. DURING INSPECTION, A WIRE WAS FOUND TO BE BROKEN IN AN EMERGENCY LIGHT. MX REPLACED THE LIGHT AND NO FURTHER DEFECTS HAVE BEEN NOTED.
- [SDR CHQA20130705257](https://openairdocs.org/sdr/CHQA20130705257), Jul 5, 2013: INVERTER. INOPERATIVE. DURING INSPECTION, RT EMERGENCY EXIT SIGN FOUND TO BE INOPERATIVE. MX FOUND NR 5 INVERTER TO INOPERATIVE AND REPLACED IT, OPS CHECKED GOOD.
- [SDR CHQA20130627234](https://openairdocs.org/sdr/CHQA20130627234), Jun 27, 2013: WINDSHIELD. CRACKED. CREW REPORTED THAT DURING CLIMB OUT, THE F/O WINDOW CRACKED. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED. MX REPLACED THE RT WI
- [SDR CHQA20130623231](https://openairdocs.org/sdr/CHQA20130623231), Jun 23, 2013: SIGN. INOPERATIVE. DURING INSPECTION, THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MX REPLACED THE SIGN AND OPS CHECKED GOOD. NO FURTHER DEFECTS WER
- [SDR CHQA20130623230](https://openairdocs.org/sdr/CHQA20130623230), Jun 23, 2013: BATTERY. INOPERATIVE. DURING INSPECTION, THE FIRST THREE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 2 BATTERY. OPS CHECKED GOOD AND NO FURTHER DEFECTS WERE NOT
- [SDR CHQA20130409108](https://openairdocs.org/sdr/CHQA20130409108), Apr 9, 2013: ANTENNA. FAILED. DURING APPROACH, CREW REPORTED ILS 1 AND 2 ERRATIC. DIVERTED AND LANDED WITHOUT INCIDENT. VOR/ILS STABILIZER ANTENNA 1 AND 2 WERE REPLACED. OPS CHECKED GOOD.
- [SDR CHQA20130406109](https://openairdocs.org/sdr/CHQA20130406109), Apr 6, 2013: FITTING. CRACKED. MAINTENANCE FOUND A CRACK IN THE SHEAR CLIP IN FRAME 28 BETWEEN STRINGERS 15R AND 16R. A REPLACEMENT SHEAR CLIP WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH 
- [SDR CHQA20130314079](https://openairdocs.org/sdr/CHQA20130314079), Mar 14, 2013: LIGHT. INOPERATIVE. CREW REPORTED THAT THE FIRST THREE EMERGENCY LIGHT PROXIMITY STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD FLOOR EMERGENCY LIGHTING STRI
- [SDR CHQA20121103405](https://openairdocs.org/sdr/CHQA20121103405), Nov 3, 2012: SIGN. INOPERATIVE. DURING INSPECTION, THE EMERGENCY EXIT SIGN ABOVE SEAT 12F WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN AT ROW 12, OPERATIONAL CHECK
- [SDR CHQA20120516172](https://openairdocs.org/sdr/CHQA20120516172), May 16, 2012: BEAM. CORRODED. DURING INSPECTION, THE CENTER FUSELAGE I RIGHT BEAM AT FRAME 22 WAS FOUND TO BE CORRODED. THE CENTER FUSELAGE RIGHT BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-
- [SDR CHQA20120516171](https://openairdocs.org/sdr/CHQA20120516171), May 16, 2012: FRAME. CRACKED. DURING INSPECTION, FRAME 66 WAS FOUND TO BE CRACKED UNDER THE LOWER BEAM. FRAME 66, UNDER THE LOWER BEAM, WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-007135.
- [SDR CHQA20120514177](https://openairdocs.org/sdr/CHQA20120514177), May 14, 2012: SKIN. DAMAGED. DURING INSPECTION, A SKIN BURN FROM A LIGHTNING STRIKE WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 30 AND FRAME 31 AT STRINGER 16R. THE RIGHT FUSELAGE SK
- [SDR CHQA20120514176](https://openairdocs.org/sdr/CHQA20120514176), May 14, 2012: SKIN. BURNED. DURING INSPECTION, A SKIN BURN FROM A LIGHTNING STRIKE WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 24 AND FRAME 25 AT STRINGER 18R. THE RIGHT FUSELAGE SK
- [SDR CHQA20120514175](https://openairdocs.org/sdr/CHQA20120514175), May 14, 2012: SHEAR PLATE. CORRODED. DURING INSPECTION, THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE FOUND TO BE CORRODED. THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE R
- [SDR CHQA20120514174](https://openairdocs.org/sdr/CHQA20120514174), May 14, 2012: SHEAR PLATE. CORRODED. DURING INSPECTION, THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE FOUND TO BE CORRODED. THE FORWARD AND AFT L-SHAPES ON THE CARGO DOOR CUTOUT WERE R
- [SDR CHQA20120514170](https://openairdocs.org/sdr/CHQA20120514170), May 14, 2012: FRAME. CRACKED. DURING INSPECTION, THE RIGHT FRAME 10 WAS FOUND TO BE CRACKED. THE RIGHT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH
- [SDR CHQA20120514169](https://openairdocs.org/sdr/CHQA20120514169), May 14, 2012: FRAME. CRACKED. DURING INSPECTION, THE LEFT FRAME 10 WAS FOUND TO BE CRACKED. THE LEFT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH S
- [SDR CHQA20120514168](https://openairdocs.org/sdr/CHQA20120514168), May 14, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE CENTER FUSELAGE I LEFT INBOARD OMEGA BEAM HAD AN EXISTING REPAIR THAT WAS FOUND TO BE CORRODED AT FRAME 20. THE CENTER FUSELAGE I LEFT IN
- [SDR CHQA20120514167](https://openairdocs.org/sdr/CHQA20120514167), May 14, 2012: BEAM. CORRODED. DURING INSPECTION, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS REPLACED. THE NEW PART WAS INSTALLED W
- [SDR CHQA20120513166](https://openairdocs.org/sdr/CHQA20120513166), May 13, 2012: FLOOR SUPPORT. CRACKED. DURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORD
- [SDR CHQA20120513165](https://openairdocs.org/sdr/CHQA20120513165), May 13, 2012: FLOOR SUPPORT. CRACKED. DURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORD
- [SDR CHQA20120513164](https://openairdocs.org/sdr/CHQA20120513164), May 13, 2012: FLOOR SUPPORT. CRACKED. DURING INSPECTION, THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDAN
- [SDR CHQA20120513163](https://openairdocs.org/sdr/CHQA20120513163), May 13, 2012: FLOOR SUPPORT. CRACKED. DURING INSPECTION, THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. THE CENTER FUSELAGE III LEFT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDAN
- [SDR CHQA20120322087](https://openairdocs.org/sdr/CHQA20120322087), Mar 22, 2012: LIGHT. INOPERATIVE. DURING INSPECTION, THE HAND RAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE HAND RAIL EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE G
- [SDR CHQA201100396](https://openairdocs.org/sdr/CHQA201100396), Oct 2, 2011: O-RING. LEAKING. CREW REPORTED, RECEIVED A BLEED 1 LEAK MESSAGE DURING CLIMB. THE AIRCRAFT RETURNED TO KCLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RINGS AT JOIN
- [SDR CHQA201000170](https://openairdocs.org/sdr/CHQA201000170), Aug 29, 2010: CLAMP. LOOSE. WHILE CLIMBING OUT OF MKE, THE CREW NOTICED THAT THE CABIN ALTITUDE RATE WAS THE SAME AS THE AIRCRAFT. THE AIRCRAFT WAS LEVELED AT 13,000FT WITH A DIFFERENTIAL 
- [SDR CHQA201000169](https://openairdocs.org/sdr/CHQA201000169), Aug 28, 2010: CONTROLLER. FAULTY. WHILE CLIMBING OUT OF MKE, THE CREW REPORTED THAT AT AROUND 14,000FT THE CABIN ALTITUDE WAS NEARING 10,000FT WITH AUTO PRESSURIZATION. THE AIRCRAFT DESCENDED TO
- [SDR CHQA201000137](https://openairdocs.org/sdr/CHQA201000137), Jul 8, 2010: WIRE. BROKEN. DURING INSPECTION, A FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REPLACED THE FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12.
- [SDR CHQA201000136](https://openairdocs.org/sdr/CHQA201000136), Jul 7, 2010: WIRE. MISSING. DURING INSPECTION, THE EMERGENCY EXIT DOOR LIGHTED PROXIMITY LIGHT STRIP WAS FOUND TO BE MISSING WIRES. MAINTENANCE REPLACED THE PROXIMITY PHOTO-LUMINESCENT LIG
- [SDR CHQA200900120](https://openairdocs.org/sdr/CHQA200900120), May 2, 2009: LIGHT. INOPERATIVE. DURING INSPECTION THE FLOOR PROXIMITY LIGHTS 6, 7, AND 8 WERE FOUND TO BE INOPERATIVE WHEN TESTED. THE NR 8 FLOOR PROXIMITY LIGHT STRIP WAS REPLACED AND LIGHTS 
- [SDR CHQA200900086](https://openairdocs.org/sdr/CHQA200900086), Mar 20, 2009: BATTERY PACK. DISCHARGED. DURING INSPECTION MAINTENANCE FOUND THE FLOOR LIGHT STRIPS 6, 7, AND 8 INOPERATIVE WHEN TESTING THE EMERGENCY LIGHT SYSTEM. THE NR 4 EMERGENCY LIGHT BATTERY WAS
- [SDR CHQA200900035](https://openairdocs.org/sdr/CHQA200900035), Jan 26, 2009: SWITCH. MALFUNCTIONED. WITH PACK 2 ON DEFERRAL AND E2 ANTI-ICE BLEED SECURED OPEN AND T/O POWER TAKEOFF WAS REQUIRED. AFTER DEPARTURE PACK NR 1 SHUTDOWN DUE TO OVERHEAT. THE QRH WAS F
- [SDR CHQA200800134](https://openairdocs.org/sdr/CHQA200800134), Jul 8, 2008: INDICATION SYS. MALFUNCTIONED. FLIGHT 3043, LGA TO IND. DURING CLIMBOUT OF LGA THE FLT CREW RECEIVED A HYDRAULIC 1 LOW QUANTITY EICAS MESSAGE. THE HYDRAULIC QUANTITY INDICATED AT THE TOP OF T
- [SDR CHQA200600142](https://openairdocs.org/sdr/CHQA200600142), Dec 27, 2006: ECU. FAILED. FLIGHT 3163 - BOS-ROC - CLIMBING OUT AT APPROXIMATELY FL200, RECEIVED "FLAP FAIL" AND "SPS ADVANCED". FLAPS STUCK AT 0 DEGREES, HIGH SPEED LANDING IN BOS. DECLA
- [SDR CHQA200600030](https://openairdocs.org/sdr/CHQA200600030), Feb 28, 2006: WIRE. BROKEN. AIRSTAIR EMERGENCY LIGHT CONNECTION (BLUE RUBBER ONE) HAS A BROKEN WIRE. REPAIRED AIRSTAIRS LIGHT WIRE IAW EMB 145 MM 20-21-00. OPS CHECK GOOD AT THIS TIME.
- [SDR CHQA200500108](https://openairdocs.org/sdr/CHQA200500108), Jun 7, 2005: ODOR. DETECTED. FLIGHT 3049 DCA-GSO - AFTER TAKEOFF, CAPTAIN AND FIRST OFFICER DETECTED A BURNING ODOR IN THE COCKPIT AND CABIN. CYCLED BOTH BLEED SYSTEMS AND ODOR WENT AWAY. M

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20051021033279I](https://openairdocs.org/incident/20051021033279I), Oct 21, 2005: Emb EMB145LR (N282SK), Rochester, NY. (-23) On October 21, 2005 at approximately 1021 local time there was an unruly passenger on chautauqua airlines flight 3155 from boston, MA. To Rochester, NY.…

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